IL269004A - Hydrogen after burner - Google Patents

Hydrogen after burner

Info

Publication number
IL269004A
IL269004A IL26900419A IL26900419A IL269004A IL 269004 A IL269004 A IL 269004A IL 26900419 A IL26900419 A IL 26900419A IL 26900419 A IL26900419 A IL 26900419A IL 269004 A IL269004 A IL 269004A
Authority
IL
Israel
Prior art keywords
burner
hydrogen
Prior art date
Application number
IL26900419A
Other languages
Hebrew (he)
Original Assignee
Eviation Tech Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Eviation Tech Ltd filed Critical Eviation Tech Ltd
Publication of IL269004A publication Critical patent/IL269004A/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60DVEHICLE CONNECTIONS
    • B60D1/00Traction couplings; Hitches; Draw-gear; Towing devices
    • B60D1/48Traction couplings; Hitches; Draw-gear; Towing devices characterised by the mounting
    • B60D1/488Traction couplings; Hitches; Draw-gear; Towing devices characterised by the mounting mounted directly to the chassis of the towing vehicle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/20Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/22Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products the fuel or oxidant being gaseous at standard temperature and pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02Aircraft characterised by the type or position of power plant
    • B64D27/24Aircraft characterised by the type or position of power plant using steam, electricity, or spring force
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/28Regulating systems responsive to plant or ambient parameters, e.g. temperature, pressure, rotor speed
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60DVEHICLE CONNECTIONS
    • B60D1/00Traction couplings; Hitches; Draw-gear; Towing devices
    • B60D1/01Traction couplings or hitches characterised by their type
    • B60D1/06Ball-and-socket hitches, e.g. constructional details, auxiliary devices, their arrangement on the vehicle
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60DVEHICLE CONNECTIONS
    • B60D1/00Traction couplings; Hitches; Draw-gear; Towing devices
    • B60D1/48Traction couplings; Hitches; Draw-gear; Towing devices characterised by the mounting
    • B60D1/52Traction couplings; Hitches; Draw-gear; Towing devices characterised by the mounting removably mounted
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B60VEHICLES IN GENERAL
    • B60DVEHICLE CONNECTIONS
    • B60D1/00Traction couplings; Hitches; Draw-gear; Towing devices
    • B60D1/58Auxiliary devices
    • B60D1/60Covers, caps or guards, e.g. comprising anti-theft devices
IL26900419A 2017-03-01 2019-08-29 Hydrogen after burner IL269004A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US201762465182P 2017-03-01 2017-03-01
PCT/IL2018/050224 WO2018158767A1 (en) 2017-03-01 2018-02-28 Hydrogen after burner

Publications (1)

Publication Number Publication Date
IL269004A true IL269004A (en) 2019-10-31

Family

ID=84286303

Family Applications (1)

Application Number Title Priority Date Filing Date
IL26900419A IL269004A (en) 2017-03-01 2019-08-29 Hydrogen after burner

Country Status (4)

Country Link
US (1) US20200023989A1 (en)
EP (1) EP3590143A4 (en)
IL (1) IL269004A (en)
WO (1) WO2018158767A1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102020113994A1 (en) 2020-05-26 2021-12-02 Audi Aktiengesellschaft Fuel cell vehicle and method for operating a fuel cell vehicle
DE102021127893A1 (en) 2021-10-26 2023-04-27 KAHLE GmbH aircraft engine

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3103324A (en) * 1953-01-23 1963-09-10 Lockheed Aircraft Corp High velocity high altitude v.t.o.l. aircraft
US7150143B2 (en) * 2003-07-21 2006-12-19 General Electric Company Hybrid fuel cell-pulse detonation power system
JP2005158283A (en) * 2003-11-20 2005-06-16 Nissan Motor Co Ltd Gas combustion device
US7966830B2 (en) * 2006-06-29 2011-06-28 The Boeing Company Fuel cell/combustor systems and methods for aircraft and other applications
JP2008016350A (en) * 2006-07-06 2008-01-24 Toyota Motor Corp Fuel cell system
CA2739492A1 (en) 2008-09-23 2010-04-08 Aerovironment Inc. Powerplant and related control system and method
US8182222B2 (en) * 2009-02-12 2012-05-22 Hamilton Sundstrand Corporation Thermal protection of rotor blades
EP2965372A1 (en) * 2013-03-08 2016-01-13 Zodiac Aerotechnics Aircraft fuel cell system with catalytic burner system
EP2878795B8 (en) * 2013-11-27 2016-10-12 Airbus Operations GmbH Engine for propelling an aircraft and aircraft having at least one engine and at least one hydrogen tank

Also Published As

Publication number Publication date
EP3590143A4 (en) 2020-12-02
US20200023989A1 (en) 2020-01-23
EP3590143A1 (en) 2020-01-08
WO2018158767A1 (en) 2018-09-07

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